Airfoil: E387 (E) Builder: Y. Tinel Comment: clean Number of Reynolds #'s: 7 Average Reynolds #: 100064 Number of angles of attack: 61 alpha / Cl / Cm -10.21 -0.454 0.0268 -9.21 -0.467 0.0234 -8.19 -0.472 0.0173 -7.19 -0.439 0.0027 -6.19 -0.393 -0.0218 -5.20 -0.326 -0.0559 -4.20 -0.186 -0.0727 -3.20 -0.047 -0.0909 -2.20 0.110 -0.1038 -1.16 0.216 -0.0868 -0.11 0.327 -0.0924 0.96 0.429 -0.0796 1.98 0.530 -0.0802 2.94 0.623 -0.0908 4.02 0.730 -0.0836 5.03 0.836 -0.0831 6.05 0.951 -0.0762 7.14 1.045 -0.0583 8.13 1.149 -0.0707 9.16 1.207 -0.0593 10.15 1.221 -0.0581 11.19 1.230 -0.0518 12.19 1.234 -0.0502 13.17 1.226 -0.0456 14.16 1.214 -0.0565 15.08 1.083 -0.1464 16.01 1.058 -0.1700 16.99 1.068 -0.1840 18.02 1.056 -0.1934 18.97 1.022 -0.1904 19.96 1.034 -0.2045 19.46 1.036 -0.2031 18.46 1.008 -0.1937 17.53 1.065 -0.1895 16.52 1.096 -0.1864 15.51 1.100 -0.1752 14.63 1.228 -0.1395 13.65 1.234 -0.0609 12.66 1.242 -0.0424 11.65 1.255 -0.0421 10.65 1.244 -0.0458 9.63 1.236 -0.0534 8.63 1.204 -0.0702 7.62 1.118 -0.0657 6.61 1.018 -0.0860 5.49 0.902 -0.0830 4.53 0.806 -0.0806 3.50 0.698 -0.0853 2.44 0.601 -0.1043 1.40 0.499 -0.0918 0.41 0.408 -0.0917 -0.60 0.301 -0.0948 -1.70 0.193 -0.0983 -2.69 0.067 -0.0942 -3.72 -0.088 -0.0802 -4.75 -0.230 -0.0764 -5.68 -0.342 -0.0431 -6.73 -0.403 -0.0265 -7.74 -0.451 -0.0007 -8.71 -0.455 0.0142 -9.67 -0.454 0.0160 Tabulated from data in file bm05140.dat & reduced using program C08.10 Average Reynolds #: 200083 Number of angles of attack: 61 alpha / Cl / Cm -10.14 -0.495 0.0488 -9.26 -0.495 0.0412 -8.25 -0.470 0.0278 -7.21 -0.425 0.0033 -6.08 -0.331 -0.0405 -5.08 -0.142 -0.0880 -4.22 -0.035 -0.0917 -3.22 0.055 -0.0869 -2.04 0.171 -0.0891 -1.09 0.253 -0.0842 -0.00 0.367 -0.0852 0.99 0.467 -0.0852 1.93 0.563 -0.0827 3.01 0.670 -0.0837 4.00 0.766 -0.0817 5.12 0.882 -0.0817 6.15 0.986 -0.0797 7.17 1.088 -0.0779 8.18 1.160 -0.0725 9.15 1.207 -0.0667 10.11 1.222 -0.0592 11.17 1.222 -0.0548 12.22 1.227 -0.0561 13.24 1.224 -0.0591 14.03 1.219 -0.0636 15.08 1.158 -0.1473 15.98 1.149 -0.1732 16.95 1.061 -0.1702 18.03 1.055 -0.1743 18.95 1.079 -0.1801 19.96 1.048 -0.1789 19.44 1.061 -0.1795 18.41 1.049 -0.1763 17.52 1.054 -0.1716 16.50 1.068 -0.1722 15.49 1.137 -0.1617 14.59 1.272 -0.1096 13.61 1.221 -0.0614 12.63 1.224 -0.0564 11.70 1.225 -0.0564 10.62 1.224 -0.0565 9.61 1.220 -0.0637 8.66 1.186 -0.0706 7.61 1.132 -0.0764 6.57 1.035 -0.0791 5.56 0.939 -0.0814 4.49 0.823 -0.0816 3.46 0.720 -0.0824 2.51 0.623 -0.0843 1.44 0.518 -0.0850 0.47 0.416 -0.0856 -0.62 0.305 -0.0848 -1.62 0.211 -0.0867 -2.63 0.115 -0.0862 -3.65 0.023 -0.0914 -4.70 -0.077 -0.0923 -5.67 -0.258 -0.0603 -6.65 -0.396 -0.0129 -7.66 -0.444 0.0180 -8.63 -0.470 0.0331 -9.69 -0.489 0.0443 Tabulated from data in file bm04978.dat & reduced using program C10.20 Average Reynolds #: 300096 Number of angles of attack: 47 alpha / Cl / Cm -8.19 -0.488 0.0273 -7.24 -0.438 -0.0010 -6.19 -0.313 -0.0492 -5.22 -0.151 -0.0828 -4.22 -0.043 -0.0841 -3.18 0.057 -0.0836 -2.07 0.174 -0.0840 -1.14 0.263 -0.0843 -0.10 0.368 -0.0827 0.94 0.480 -0.0832 1.98 0.592 -0.0831 2.99 0.692 -0.0828 4.06 0.802 -0.0825 5.03 0.905 -0.0817 6.08 1.013 -0.0806 7.08 1.104 -0.0779 8.16 1.182 -0.0732 9.19 1.223 -0.0667 10.15 1.239 -0.0597 11.15 1.247 -0.0576 12.13 1.243 -0.0572 13.17 1.247 -0.0619 14.04 1.291 -0.0862 15.02 1.273 -0.1327 14.65 1.281 -0.1233 13.65 1.245 -0.0657 12.64 1.244 -0.0597 11.62 1.249 -0.0580 10.65 1.242 -0.0584 9.69 1.233 -0.0640 8.62 1.209 -0.0716 7.59 1.142 -0.0768 6.58 1.061 -0.0806 5.61 0.962 -0.0821 4.58 0.861 -0.0832 3.55 0.745 -0.0835 2.50 0.636 -0.0836 1.43 0.530 -0.0835 0.45 0.427 -0.0836 -0.56 0.320 -0.0831 -1.62 0.214 -0.0846 -2.64 0.112 -0.0841 -3.70 0.006 -0.0840 -4.74 -0.095 -0.0848 -5.78 -0.230 -0.0711 -6.67 -0.390 -0.0232 -7.68 -0.464 0.0128 Tabulated from data in file bm04980.dat & reduced using program C10.20 Average Reynolds #: 350282 Number of angles of attack: 47 alpha / Cl / Cm -8.20 -0.492 0.0246 -7.20 -0.439 -0.0015 -6.23 -0.308 -0.0513 -5.19 -0.156 -0.0818 -4.19 -0.046 -0.0833 -3.16 0.060 -0.0832 -2.15 0.167 -0.0838 -1.10 0.270 -0.0848 -0.07 0.375 -0.0827 0.92 0.477 -0.0830 1.99 0.589 -0.0832 3.02 0.707 -0.0834 4.03 0.813 -0.0824 5.04 0.916 -0.0819 6.05 1.021 -0.0810 7.09 1.112 -0.0777 8.15 1.177 -0.0727 9.15 1.223 -0.0665 10.14 1.246 -0.0598 11.17 1.251 -0.0578 12.12 1.251 -0.0592 13.16 1.252 -0.0633 14.11 1.302 -0.0827 14.78 1.303 -0.1250 14.64 1.290 -0.1148 13.64 1.252 -0.0661 12.64 1.253 -0.0616 11.66 1.256 -0.0590 10.66 1.249 -0.0584 9.65 1.235 -0.0629 8.62 1.206 -0.0702 7.66 1.152 -0.0757 6.59 1.067 -0.0797 5.57 0.968 -0.0817 4.58 0.863 -0.0827 3.49 0.754 -0.0840 2.47 0.639 -0.0833 1.44 0.532 -0.0838 0.38 0.418 -0.0835 -0.59 0.316 -0.0835 -1.63 0.217 -0.0846 -2.66 0.107 -0.0839 -3.65 0.007 -0.0831 -4.70 -0.097 -0.0840 -5.73 -0.232 -0.0710 -6.69 -0.377 -0.0300 -7.68 -0.475 0.0128 Tabulated from data in file bm04982.dat & reduced using program C10.20 Average Reynolds #: 349714 Number of angles of attack: 21 alpha / Cl / Cm 10.21 1.248 -0.0201 11.19 1.255 -0.0202 12.23 1.260 -0.0203 13.14 1.258 -0.0202 14.19 1.308 -0.0210 15.06 1.272 -0.0205 16.05 1.201 -0.0193 17.28 1.122 -0.0181 18.18 1.072 -0.0172 19.19 1.059 -0.0170 20.12 1.063 -0.0171 19.63 1.055 -0.0170 18.65 1.053 -0.0169 17.69 1.115 -0.0179 16.67 1.168 -0.0188 15.64 1.257 -0.0202 14.69 1.326 -0.0213 13.63 1.253 -0.0202 12.66 1.255 -0.0202 11.75 1.261 -0.0203 10.68 1.252 -0.0201 Tabulated from data in file bm05121.dat & reduced using program C10.20 Average Reynolds #: 460154 Number of angles of attack: 43 alpha / Cl / Cm -7.16 -0.425 -0.0069 -6.22 -0.310 -0.0514 -5.23 -0.166 -0.0795 -4.15 -0.046 -0.0818 -3.14 0.057 -0.0820 -2.12 0.163 -0.0828 -1.11 0.264 -0.0833 -0.07 0.369 -0.0820 0.98 0.484 -0.0819 1.98 0.594 -0.0819 3.02 0.710 -0.0820 4.03 0.819 -0.0813 5.06 0.925 -0.0804 6.07 1.025 -0.0793 7.12 1.106 -0.0756 8.13 1.189 -0.0717 9.16 1.234 -0.0658 10.14 1.253 -0.0596 11.19 1.260 -0.0593 12.17 1.260 -0.0625 13.15 1.269 -0.0661 14.12 1.261 -0.0728 13.65 1.258 -0.0696 12.62 1.270 -0.0656 11.61 1.264 -0.0612 10.68 1.252 -0.0588 9.66 1.253 -0.0626 8.63 1.208 -0.0689 7.60 1.154 -0.0740 6.54 1.072 -0.0779 5.54 0.975 -0.0801 4.57 0.874 -0.0812 3.52 0.759 -0.0813 2.46 0.650 -0.0820 1.48 0.538 -0.0819 0.44 0.423 -0.0816 -0.60 0.317 -0.0834 -1.62 0.213 -0.0834 -2.65 0.106 -0.0817 -3.68 0.000 -0.0823 -4.71 -0.101 -0.0821 -5.73 -0.233 -0.0707 -6.65 -0.363 -0.0333 Tabulated from data in file bm04984.dat & reduced using program C10.20 Average Reynolds #: 499909 Number of angles of attack: 43 alpha / Cl / Cm -7.26 -0.434 -0.0026 -6.23 -0.307 -0.0513 -5.25 -0.171 -0.0786 -4.22 -0.049 -0.0815 -3.15 0.057 -0.0819 -2.10 0.166 -0.0822 -1.12 0.265 -0.0826 -0.06 0.377 -0.0812 0.99 0.491 -0.0815 1.92 0.590 -0.0810 3.00 0.712 -0.0813 4.04 0.816 -0.0807 5.04 0.927 -0.0804 6.08 1.026 -0.0789 7.12 1.118 -0.0758 8.14 1.183 -0.0712 9.17 1.240 -0.0660 10.14 1.258 -0.0593 11.19 1.269 -0.0597 12.21 1.269 -0.0632 13.14 1.268 -0.0682 14.15 1.264 -0.0741 13.63 1.264 -0.0714 12.63 1.261 -0.0645 11.63 1.259 -0.0592 10.63 1.256 -0.0578 9.63 1.243 -0.0614 8.63 1.205 -0.0677 7.59 1.134 -0.0723 6.60 1.078 -0.0774 5.58 0.979 -0.0795 4.52 0.861 -0.0797 3.44 0.755 -0.0810 2.51 0.649 -0.0806 1.42 0.535 -0.0810 0.43 0.426 -0.0813 -0.62 0.320 -0.0831 -1.65 0.209 -0.0825 -2.67 0.108 -0.0820 -3.68 0.002 -0.0811 -4.71 -0.107 -0.0819 -5.75 -0.236 -0.0698 -6.73 -0.370 -0.0334 Tabulated from data in file bm04986.dat & reduced using program C10.20 File e387_c.lft created using program C10.20 on Thu May 22 17:01:21 2003